An oblique shock wave at an angle of 35 degrees occurs at leading edge of a symmetrical wedge. Air has a Mach number of 2 and pressure and temperature of 10 bar and 310 K respectively upstream of the wave. Determine the wedge angle and pressure, temperature and Mach number downstream of the wave.
An oblique shock wave at an angle of 35 degrees occurs at leading edge of a symmetrical wedge. Air has a Mach number of 2 and pressure and temperature of 10 bar and 310 K respectively upstream of the wave. Determine the wedge angle and pressure, temperature and Mach number downstream of the wave.
Sustainable Energy
2nd Edition
ISBN:9781337551663
Author:DUNLAP, Richard A.
Publisher:DUNLAP, Richard A.
Chapter12: Wave Energy
Section: Chapter Questions
Problem 3P
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An oblique shock wave at an angle of 35 degrees occurs at leading edge of a symmetrical wedge. Air has a Mach number of 2 and pressure and temperature of 10 bar and 310 K respectively upstream of the wave. Determine the wedge angle and pressure, temperature and Mach number downstream of the wave.
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